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Simulations of an aeroelastic control system for shock/boundary layer interactions
S. T. McIlwain
, J. Y. Kim
, S. Breitenfeld
, E. Loth
,
P. H. Geubelle
, D. Torterelli
Aerospace Engineering
National Center for Supercomputing Applications (NCSA)
Mechanical Science and Engineering
Grainger College of Engineering
Beckman Institute for Advanced Science and Technology
Research output
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peer-review
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Keyphrases
Control System
100%
Free Stream
100%
Aeroelastic Control
100%
SWBLI
100%
Cavity Volume
66%
Oblique Shock Wave
66%
Pressure Difference
33%
Deformable
33%
Computational Fluid Dynamics
33%
Parallelization
33%
Flap
33%
Surface Boundary Layer
33%
Result Comparison
33%
Optimization Analysis
33%
CFD Code
33%
Transpiration
33%
Cavity Pressure
33%
Thin Flap
33%
Dynamic Code
33%
Engineering
Control System
100%
Boundary Layer
100%
Layer Interaction
100%
Aeroelastic Control
100%
Computational Fluid Dynamics
66%
Flaps
66%
Oblique Shock
66%
Pressure Difference
33%
Freestream Flow
33%
Cavity Pressure
33%
Surface Boundary
33%
Physics
Boundary Layer
100%
Computational Fluid Dynamics
66%
Oblique Shock Wave
66%
Shock Wave
33%
Charge Flow Device
33%